Technical Field
[0001] The present invention relates to: a carbon fiber precursor fiber using a novel heat-resistant
aromatic polymer and not needing an infusibilization treatment (a pre-treatment including
a flame resistance-imparting treatment); a carbon fiber; and a method for producing
a carbon fiber.
Background Art
[0002] Carbon fibers have been used in a wide variety of applications from aircraft to building
materials. If their productivity is improved and their cost is lowered more and more,
they can be materials in place of stainless steel plates also in automobile body and
the like. At present, carbon fibers are mainly produced using polyacrylonitrile (PAN)
fibers and pitch fibers as raw materials (carbon fiber precursor fibers).
[0003] These carbon fiber precursor fibers, however, need a pre-treatment called an infusibilization
treatment prior to carbonization, and this treatment is a major barrier to reduction
in cost and energy required for their production, and to increase in productivity.
[0004] Specifically, since PAN fibers and pitch fibers are fused in the course of a carbonization
treatment (a high-temperature thermal treatment at 1,000°C or higher) and cannot maintain
their fiber shapes, they are changed to infusible, flame-resistant fibers by an air
oxidization treatment called an infusibilization treatment and then are subjected
to carbonization to obtain carbon fibers. In this infusibilization treatment, it is
necessary to uniformly control oxidation reaction and also strictly manage temperature
conditions for suppressing thermal runaway due to exothermic reaction.
[0005] Meanwhile, some kinds of heat-resistant aromatic polymers (e.g., aramid fibers and
phenol resin fibers) have such properties that they are carbonized without being fused,
and thus it is possible to obtain carbon fibers only by forming such polymers into
fibers and subjecting the resultant fibers to a high-temperature thermal treatment.
[0006] Although aramid fibers and phenol resin fibers are carbonized while maintaining their
fiber shape, they have problems that their mechanical strengths (e.g., tensile strength
and elastic modulus) are poor.
[0007] That is, when only carbonization is performed while shapes are being maintained,
sufficient mechanical properties (e.g., strength and elasticity) required for carbon
fiber products are not developed, and thus there is still a need to develop new materials
realizing sufficient mechanical properties.
[0008] Also, the present inventors previously found out a graphite film containing a heterocyclic
polymer obtained through condensation between an aromatic tetracarboxylic acid and
an aromatic tetraamine (see PTL 1).
[0009] However, when crystallization excessively high in two-dimensional (layer-form) orientation
occurs like in a graphite film, cracks of fibers occur due to delamination in a parallel
direction to graphite crystal layers bonded only via intermolecular force, and strength
as fibers is problematically very weak.
[0010] In view of the above, the present inventors found out a carbon fiber using poly[bis-(benzimidazobenzisoquinoline)]
(PBB) as a precursor fiber (see NPL 1). This carbon fiber (PBB carbon fiber) can be
obtained only by performing a high-temperature thermal treatment on the precursor
fiber without an infusibilization treatment, and exhibits excellent mechanical properties.
[0011] However, the PBB has not yet been a widely used material and is an expensive material
as compared with the existing precursor fibers. Thus, at present, there is a problem
in terms of cost when putting PBB carbon fibers into practice.
[0012] Meanwhile, a resin formed from a polymer material having a polyoxadine structure
as a repeating unit is known as a relatively low cost resin (see NPL 2). That is,
this polymer material is a polymer that can be synthesized using, as raw materials,
phenols, anilines, and paraformaldehyde, which are widely used as organic compound
materials, and thus it can be produced at a low cost.
[0013] However, such a polymer material has only been studied for applications to resin
films, and has not been studied for preparation in the fibrous form and formation
into carbon fibers. Thus, it has been unclear as to carbonization conditions including
an infusibilization treatment and as to mechanical strengths when it is carbonized.
Also, substances having an oxadine ring develop thermal curability through ring-opening
polymerization by a thermal treatment, and thus can be seen as one kind of a phenol
resin. Therefore, those substances are expected to have an amorphous structure with
no orientability even after carbonization, and as a result it has been considered
difficult to obtain practical carbon fiber products excellent in mechanical strengths.
In actual, monomers having an oxadine structure are practically used as a thermosetting
resin, a matrix agent for composite materials, or a sizing agent for carbon fibers.
However, no example has been reported that polymer materials having an oxadine structure
were carbonized into carbon fiber products.
Citation List
Patent Literature
Non-Patent Literature
Summary of Invention
Technical Problem
[0016] The present invention aims to solve the above existing problems and achieve the following
object. That is, an object of the present invention is to provide: a carbon fiber
precursor fiber that can efficiently produce a carbon fiber at a low cost which is
excellent in mechanical strengths even without an infusibilization treatment; a carbon
fiber; and a method for producing the carbon fiber.
Solution to Problem
[0017] Means for solving the above problems are as follows.
- <1> A carbon fiber precursor fiber, including:
a polymer containing a constituent unit represented by General Formula (1) below:

where in the General Fomula (1), X and Y each independently represent a divalent substituent,
a single bond, or a structure forming a fused ring by sharing one side of two adjacent
rings, and the divalent substituent is selected from the group consisting of -O-,
-S-, -OSO-, -NH-, -CO-, -CH2-, and -CH(CH3)2-.
- <2> The carbon fiber precursor fiber according to <1> above, further including a polymer
containing a constituent unit represented by General Formula (2) below:

where in the General Formula (2), Ar1 represents an aryl group expressed by any one of Structural Formulas (1) to (5) below,
and Ar2 represents an aryl group expressed by Structural Formula (6) or (7) below:




- <3> A carbon fiber obtained by carbonizing the carbon fiber precursor fiber according
to <1> or <2> above.
- <4> The carbon fiber according to <3> above, wherein a fiber diameter of the carbon
fiber is 1 µm or more.
- <5> A method for producing a carbon fiber, the method including:
spinning a compound to be spun containing a polymer containing a constituent unit
represented by General Formula (1) below to obtain a carbon fiber precursor fiber;
and
heating the carbon fiber precursor fiber under inert gas to carbonize the carbon fiber
precursor fiber:

where in the General Fomula (1), X and Y each independently represent a divalent substituent,
a single bond, or a structure forming a fused ring by sharing one side of two adjacent
rings, and the divalent substituent is selected from the group consisting of -O-,
-S-, -OSO-, -NH-, -CO-, -CH2-, and -CH(CH3)2-.
- <6> The method for producing a carbon fiber according to <5> above, wherein the spinning
is spinning the compound to be spun containing the polymer containing the constituent
unit represented by the General Formula (1) and a compound to be spun containing a
constituent unit represented by General Formula (2) below, to obtain a carbon fiber
precursor fiber:

where in the General Formula (2), Ar1 represents an aryl group expressed by any one of Structural Formulas (1) to (5) below,
and Ar2 represents an aryl group expressed by Structural Formula (6) or (7) below:




Advantageous Effects of Invention
[0018] According to the present invention, it is possible to solve the above existing problems
and provide a carbon fiber precursor fiber that can efficiently produce a carbon fiber
at a low cost which is excellent in mechanical strengths even without an infusibilization
treatment; a carbon fiber; and a method for producing the carbon fiber.
Brief Description of Drawings
[0019]
FIG. 1A is a scanning microscopic image of carbon fibers according to Example 1-2.
FIG. 1B is a scanning microscopic image that is enlarged in the fiber length direction
of the carbon fibers depicted in FIG. 1A.
FIG. 1C is a scanning microscopic image that is enlarged in the fiber diameter direction
of the carbon fibers depicted in FIG. 1A.
FIG. 2A is a conceptual diagram indicating plane interval c/2 of carbon network planes
and stack thickness Lc of carbon network planes in a graphite crystal.
FIG. 2B is a conceptual diagram indicating an optical system in measuring wide angle
X-ray diffraction.
Description of Embodiments
(Carbon Fiber Precursor Fiber and Method for Producing the Same)
[0020] A carbon fiber precursor fiber of the present invention is a fibrous material containing
a polymer containing a constituent unit represented by General Formula (1) below.
[0021] The fibrous material of the polymer can be carbonized as is without an infusibilization
treatment. Also, it can have sufficient mechanical strengths when carbonized with
a thermal treatment. One possible reason for this is as follows. Specifically, as
represented in the General Formula (1), the polymer has a rod-like aromatic polymer
structure at the stage before formed into a fiber. With this structure, the polymer
has such a property that the molecules will easily be arranged in the fiber axis direction
by the action of stress which the polymer chains will receive upon spinning. Once
such a property has been imparted thereto upon the spinning, development of graphite
crystals is made possible upon the carbonization while maintaining the fiber axis
orientability. In addition, the cross-linked structure between the polymer chains
through ring-opening polymerization unique to an oxazine ring (a heterocycle containing
O and N atoms) makes it possible to allow the carbon fiber tissue structure to have
an appropriate level of a non-crystalline structure which is necessary for increasing
the strength of carbon fibers.

[0022] In the General Fomula (1), X and Y each independently represent a divalent substituent,
a single bond, or a structure forming a fused ring by sharing one side of two adjacent
rings, and the divalent substituent is selected from the group consisting of -O-,
-S-, -OSO-, -NH-, -CO-, -CH
2-, and -CH(CH
3)
2-.
[0023] The polymer containing the constituent unit represented by the General Formula (1)
can be synthesized by the following method.
[0024] Specifically, the above polymer can be obtained through reaction between the following
starting materials: an aromatic dihydroxy compound represented by General Formula
(3) below or a derivative of the aromatic dihydroxy compound such as an acid chloride
thereof, an acid anhydride thereof, an ester thereof, or an amide thereof an aromatic
diamine represented by General Formula (4) below or a salt thereof; and paraformaldehyde.

[0025] In the General Formulas (3) and (4), X and Y each independently represent a divalent
substituent, a single bond, or a structure forming a fused ring by sharing one side
of two adjacent rings, and the divalent substituent is selected from the group consisting
of -O-, -S-, -OSO-, -NH-, -CO-, -CH
2-, and -CH(CH
3)
2-.
[0026] Specific examples of the aromatic dihydroxy compound include 4,4-dihydroxydiphenyl
ether, bis(4-hydroxyphenyl)methane, bis(4-hydroxyphenyl)sulfide, bis(4-hydroxyphenyl)sulfone,
bis(4-hydroxyphenyl)amine, 4'4-dihydroxybenzophenone, and 2,2,-bis(4-hydroxyphenyl)propane.
Specific examples of the aromatic diamine compound include 4,4-diaminodiphenyl ether
(which is also called 4,4-oxydianiline), bis(4-aminophenyl)sulfide, bis(4-aminophenyl)sulfone,
bis(4-aminophenyl)amine, 4'4-diaminobenzophenone, and 2,2,-bis(4-aminophenyl)propane.
[0027] Examples of the structure forming a fused ring by sharing one side of two adjacent
rings in X or Y in the General Formula (3) or (4) include a structure where the two
adjacent rings form a naphthalene ring. In this case, the structures of X and Y are
introduced into the constituent unit represented by the General Formula (1) as the
structures of X and Y in the General Formula (1).
[0028] A polymerizing method for obtaining the polymer is, for example, as follows. Specifically,
the aromatic dihydroxy compound or the derivative thereof and the aromatic diamine
or the salt thereof are added to a reaction vessel containing the paraformaldehyde
and a solvent. In chloroform, the resultant mixture is stirred and refluxed for 3
hours to 48 hours, to obtain the polymer containing the constituent unit represented
by the General Formula (1).
[0029] The solvent is not particularly limited so long as it is a solvent that can dissolve
the starting materials and does not prevent the polymerization. Specific examples
of the solvent include chloroform, methanol, benzene, and toluene.
[0030] These compounds used as starting materials for the synthesis of the polymer may be
synthesized by known methods or may be commercially available products that are purchased.
[0031] The carbon fiber precursor may be a fibrous material obtained from the polymer itself
containing the constituent unit represented by the General Formula (1) as a repeating
unit, but so long as the effects of the present invention are not impeded, the carbon
fiber precursor may also be a fibrous material obtained from the above polymer having
the end to which any substituent has been added.
[0032] Examples of the substituent include an ester group, an amide group, an imide group,
a hydroxyl group, and a nitro group.
[0033] The number of the repeating units of the constituent unit represented by the General
Formula (1) is about 100 to about 100,000.
[0034] The carbon fiber precursor fiber can be produced by spinning a compound to be spun
(polymer) containing the polymer containing the constituent unit represented by the
General Formula (1).
[0035] An intrinsic viscosity of the compound to be spun is not particularly limited but
is preferably 0.05 dL·g
-1 to 5 dL·g
-1.
[0036] When the intrinsic viscosity thereof is less than 0.05 dL·g
-1, the fibers may be fractured during spinning. When it is more than 5 dL·g
-1, the compound to be spun may not homogeneously dissolve in the below-described solvent
used for spinning. Note that, 1 dL·g
-1 is equivalent to 10
-4 m
3·g
-1.
[0037] So long as the effects of the present invention are not impeded, the carbon fiber
precursor fiber may be a fibrous material obtained from a copolymer obtained by copolymerizing
the constituent unit represented by the General Formula (1) and another constituent
unit.
[0038] So long as the effects of the present invention are not impeded, the carbon fiber
precursor fiber may also be a fibrous material containing another polymer.
[0039] Such another polymer is not particularly limited so long as it is a polymer that
can be carbonized even without an infusibilization treatment. Examples thereof include
aromatic polyamide, polyimide, polyoxadiazole, polyimidazole, and other polymers.
Among them, the polymer containing the constituent unit represented by the General
Formula (2) is preferable from the viewpoint of increasing the mechanical strengths.

[0040] In the General Formula (2), Ar
1 represents an aryl group expressed by any one of Structural Formulas (1) to (5) below,
and Ar
2 represents an aryl group expressed by Structural Formula (6) or (7) below.

[0041] The polymer containing the constituent unit represented by the General Formula (2)
can be synthesized by the following method.
[0042] Specifically, it can be obtained by reacting, as starting materials, aromatic tetracarboxylic
acid or aromatic tetracarboxylic acid derivatives, such as acid chlorides, acid anhydrides,
esters or amides thereof, with aromatic tetraamine or salts thereof.
[0043] Examples of the aromatic tetracarboxylic acids include 1,4,5,8-naphthalenetetracarboxylic
acid and 4,4'-binaphthy-1,1',8,8'-tetracarboxylic acid. Examples of the aromatic tetraamines
include 1,2,4,5-benzenetetraamine and 3, 3',4,4'-biphenyltetraamine.
[0044] In one polymerization method employable, the aromatic tetracarboxylic acid or carboxylic
acid derivatives thereof and the aromatic tetraamine or salts thereof are added to
a reaction vessel containing a solvent, and the mixture is stirred at 100°C to 250°C
for 3 hours to 48 hours, to thereby obtain the polymer containing the constituent
unit represented by the General Formula (2) as a repeating unit.
[0045] The solvent is not particularly limited so long as it can dissolve the starting materials
and formed polymers and has an effect as a catalyst of promoting polymerization. Specific
examples thereof include polyphosphoric acid, polyphosphoric acid esters, and cresyl
diphenyl phosphate, as well as methane sulfonic acid in which diphosphorus pentoxide
or the like has been dissolved.
[0046] The 1,4,5,8-naphthalenetetracarboxylic acid can be synthesized from pyrene in 2 steps
consisting of oxidation with potassium permanganate and oxidation with sodium hypochlorite
solution. The 4,4'-binaphthy-1,1',8,8'-tetracarboxylic acid can be synthesized from
4-chloro-1,8,-naphthalic anhydride in 3 steps consisting of esterification, coupling,
and hydrolysis. The 1,2,4,5-benzenetetraamine can be synthesized from m-chlorobenzene
in 3 steps consisting of nitration, amination, and reduction of the nitro group, and
isolated and used as tetrahydrochloride thereof. The 3,3',4,4'-biphenyltetraamine
can be synthesized from o(ortho)-nitroaniline in 3 steps consisting of iodination,
cross coupling, and reduction of the amino group.
[0047] Note that, commercially available products of them may also be purchased and used.
[0048] The polymer represented by the General Formula (2) may have any substituent added
to the end thereof.
[0049] Examples of the substituent include an ester group, an amide group, an imide group,
a hydroxyl group, and a nitro group.
[0050] The number of the repeating units of the constituent unit represented by the General.
Formula (2) is about 100 to about 100,000.
[0051] When the carbon fiber precursor fiber is composed of a fibrous material containing
the polymer containing the constituent unit represented by the General Formula (1)
and the polymer containing the constituent unit represented by the General Formula
(2), a mixing ratio of the polymer containing the constituent unit represented by
the General Formula (1) and the polymer containing the constituent unit represented
by the General Formula (2) is preferably 1/3 to 3 as a mass ratio expressed by the
following formula; i.e., "the polymer containing the constituent unit represented
by the General Formula (2) / the polymer containing the constituent unit represented
by the General Formula (1)".
[0052] When the mass ratio is less than 1/3, mechanical strengths cannot sufficiently be
increased in some cases. Even when it is more than 3, mechanical strengths will remain
unchanged, and the cost will simply increase in some cases.
[0053] The carbon fiber precursor fiber can be produced by spinning compounds to be spun
including the polymer containing the constituent unit represented by the General Formula
(1) and if necessary, the polymer containing the constituent unit represented by the
General Formula (2) and the like.
[0054] A method for the spinning is not particularly limited and may be appropriately selected
depending on the intended purpose. Examples thereof include known wet-type spinning
methods and dry-type spinning methods.
[0055] A solvent used in the wet-type spinning methods and dry-type spinning methods is
not particularly limited so long as it is a solvent in which the compound to be spun
can dissolve. Examples thereof include chloroform, toluene, and methanesuofonic acid.
[0056] Also, a coagulation liquid for eluting the solvent and coagulating the compound to
be spun as the carbon fiber precursor fiber is not particularly limited. Examples
thereof include water, alcohol, and diluted sulfuric acid.
[0057] Even when the carbon fiber precursor fiber is made large in its fiber diameter, the
carbon fiber precursor fiber is not impaired in its shape upon the subsequent carbonization
treatment. The fiber diameter thereof is not particularly limited and may be appropriately
selected depending on the intended purpose. It may be 50 µm or more, if necessary.
Note that, the upper limit of the fiber diameter is about 1,000 µm.
[0058] In the preparation of the carbon fiber precursor fiber, a drawing treatment may be
performed, if necessary. As the drawing treatment, spun yarn may be drawn directly
in a coagulation bath, or wound yarn may be washed with water and then drawn in the
bath. Also, a draw ratio is preferably about 1.2 times to about 10 times.
(Carbon Fiber and Method for Producing the Same)
[0059] A carbon fiber of the present invention can be obtained by carbonizing the carbon
fiber precursor fiber. Also, a method for producing the carbon fiber includes a carbonization
step of heating the carbon fiber precursor fiber under inert gas to carbonize the
carbon fiber precursor fiber.
[0060] The inert gas is not particularly limited, and examples thereof include nitrogen
and argon gas.
[0061] A method for the heating is, for example, a method of performing pre-heating for
ring-opening polymerization of the oxazine ring of the polymer containing the constituent
unit represented by the General Formula (1) and then post-heating for carbonization
of the ring-opening polymer.
[0062] The pre-heating is not particularly limited so long as the ring-opening polymerization
reaction can proceed. However, it is preferably performed under temperature conditions
of 200°C to 600°C in a nitrogen atmosphere for the purpose of making the production
process highly efficient. When the drawing treatment is performed, this pre-heating
may be performed at the same time as the drawing treatment.
[0063] In the method for producing the carbon fiber, the post-heating in the carbonization
step can be rapidly performed.
[0064] Although conditions for the post-heating are not particularly limited, a temperature
increasing rate can be set to 5 °C/min or more. The upper limit of the temperature
increasing rate is about 500 °C/min. The temperature conditions of the post-heating
heated most are preferably 800°C to 2,000°C. Heating at such a temperature makes it
possible to carbonize the carbon fiber precursor fiber while maintaining its shape.
[0065] At this time, in the carbon fiber precursor fiber containing the polymer containing
the constituent unit represented by the General Formula (1), it is possible to moderately
perform both development of graphite crystals and impartment of a three-dimensional
crosslinked structure, which makes it possible to produce carbon fibers having sufficient
mechanical properties.
[0066] Also, in order to control the mechanical properties (e.g., strength and elasticity)
of the carbon fiber obtained by the carbonization, the method for producing the carbon
fiber may include, after the carbonization step or successively with the carbonization
step, a graphitizing step of heating the carbon fiber at a higher temperature to graphitize
the carbon fiber.
[0067] A heating temperature in the graphitizing step (a heating step to be performed successively
with the carbonization step in some cases) is not particularly limited but is preferably
2,000°C to 3,200°C. Setting the heating temperature in such a range makes it possible
to produce the carbon fibers having sufficient mechanical properties at high carbonization
yield and high density.
[0068] Note that, the graphitizing step is preferably performed under the inert gas similar
to the carbonization step.
[0069] Note that, the method for producing the carbon fiber may further include steps of
performing a surface treatment and a sizing impartment, which are performed in known
carbon fiber production processes.
[0070] By spinning the carbon fiber precursor fibers so as to be thick fibers in the spinning,
the carbon fibers can be increased in diameter while maintaining mechanical strengths.
Commercially available carbon fibers such as PAN-type carbon fibers usually have a
fiber diameter of about 7 µm. Mechanical strengths of the carbon fibers are maintained
not only in the case where the fiber diameter is 1 µm or more but less than 8 µm,
but also in the case where the fiber diameter is 8 µm or more, and even in the case
where the fiber diameter is 16 µm or more. Note that, the upper limit of the fiber
diameter is about 30 µm.
[0071] Depending on the aspect of the spinning, the carbon fibers can be formed into short
fibers (spun) or continuous fibers (filament).
Examples
(Example 1-1)
<Synthesis of polyoxazine/PBB=1/1 carbon fiber precursor fibers>
[0072] In accordance with the following Synthesis Scheme (1), equimolar amounts of bis(4-hydroxyphenyl)methane
(also called Bisphenol F, BPF, product of Tokyo Chemical Industry Co., Ltd., Distributor
Code: No. B0819) and 4,4-oxydianiline (also called 4,4-diaminodiphenyl ether, ODA,
product of Tokyo Chemical Industry Co., Ltd., Distributor Code: No. 00088) and a 4.3
times molar amount of paraformaldehyde (product of Tokyo Chemical Industry Co., Ltd.,
Distributor Code: No. P0018) were refluxed for 5 hours in chloroform (product of Wako
Pure Chemical Industries, Ltd., Distributor Code: No. 038-02606) for polycondensation,
to synthesize poly(N,N'-oxydiphenylene-4,4'-methylene dibenzoxazine) (hereinafter
abbreviated as "polyBPF/ODA oxazine"). Note that, the intrinsic viscosity of this
polyBPF/ODA oxazine was found to be 0.056 dL·g
-1.

[0073] Next, 4-chloro-1,8-naphthalic anhydride (product of Alfa Aesar Co., Distributor Code:
No. L05508) was allowed to undergo an esterification treatment, a coupling treatment,
and a hydrolysis treatment in this order in accordance with the following Synthesis
Scheme (2), to thereby synthesize 4,4'-binaphthy-1,1',8,8'-tetracarboxylic acid (hereinafter
abbreviated as "BNTCA").

[0074] Note that, "DMAc" in the Synthesis Scheme (2) means dimethyl acetoamide.
[0075] Next, in accordance with the following Synthesis Scheme (3), equimolar amounts of
BNTCA and 4,4'-biphenyl-1,1',2,2'-tetraamine (product of Aldrich Co., Distributor
Code: No. D12384, hereinafter abbreviated as "BPTA") were added to polyphosphoric
acid (product of Sigma-Aldrich Co., Distributor Code: No. 208213, hereinafter abbreviated
as "PPA") and were allowed to undergo polycondensation, to thereby synthesize poly[bis-(benzimidazoisoquinoline)]
(hereinafter abbreviated as "PBB").

[0076] Next, 25 g of the synthesized polyBPF/ODA oxazine and 25 g of PBB were dissolved
in 1 L of methanesulfonic acid (product of Wako Pure Chemical Industries, Co., Distributor
Code: No. 138-01576, hereinafter abbreviated as "MSA") to prepare a raw liquid for
spinning.
[0077] The raw liquid for spinning was introduced to a wet-type spinning device. While introduced
to a water bath serving as a coagulation bath, the raw liquid for spinning was allowed
to pass through a multihole nozzle member with 402 nozzle holes formed, and to be
discharged as a bundle of 402 fibers. After washing and drying, this was wound by
a winding device to obtain carbon fiber precursor fibers (hereinafter these spun fibers
are abbreviated as "polyoxazine/PBB=1/1 carbon fiber precursor fibers"). The obtained
polyoxazine/PBB=1/1 carbon fiber precursor fibers were found to have a fiber diameter
of about 12 µm.
<Carbonization Treatment>
[0078] The polyoxazine/PBB=1/1 carbon fiber precursor fibers were carbonized in a nitrogen
atmosphere to produce carbon fibers of Example 1-1. Specifically, for the carbonization
of the polyoxazine/PBB=1/1 carbon fiber precursor fibers, they were heated at 240°C
for 30 minutes, then were heated to 1,300°C at a temperature increasing rate of 10
°C/min, and were maintained for 10 minutes. Note that, this carbonization treatment
was performed in a state where a tension of 2 mN was applied to the polyoxazine/PBB=1/1
carbon fiber precursor fibers. The obtained carbon fibers were found to have a fiber
diameter of about 9 µm.
(Example 1-2)
[0079] Carbon fibers according to Example 1-2 were produced in the same manner as in Example
1-1 except that the carbonization temperature was changed, i.e., the polyoxazine/PBB=1/1
carbon fiber precursor fibers were carbonized by being heated at 240°C for 30 minutes
in a nitrogen atmosphere, then heated to 1,500°C at a temperature increasing rate
of 10 °C/min, and maintained for 10 minutes. The obtained carbon fibers were found
to have a fiber diameter of 9 µm. Microscopic images of the obtained carbon fibers
according to Example 1-2 are depicted in FIGs. 1A to 1C. FIG. 1A is a scanning microscopic
image of the carbon fibers according to Example 1-2. FIG. 1B is a scanning microscopic
image that is enlarged in the fiber length direction of the carbon fibers depicted
in FIG. 1A. FIG. 1C is a scanning microscopic image that is enlarged in the fiber
diameter direction of the carbon fibers depicted in FIG. 1A.
(Example 2-1)
[0080] Carbon fibers according to Example 2-1 were produced in the same manner as in Example
1-1 except that the amount of PBB added was changed; i.e., wet-type spinning was performed
using a raw liquid for spinning prepared by dissolving 25 g of the polyBPF/ODA oxazine
and 75 g of PBB in 1 L of the methanesulfonic acid (hereinafter the spun fibers are
abbreviated as "polyoxazine/PBB=1/3 carbon fiber precursor fibers"). The obtained
carbon fibers were found to have a fiber diameter of about 9 µm.
(Example 2-2)
[0081] Carbon fibers according to Example 2-2 were produced in the same manner as in Example
2-1 except that the carbonization temperature was changed, i.e., the polyoxazine/PBB=1/3
carbon fiber precursor fibers were carbonized by being heated at 240°C for 30 minutes
in a nitrogen atmosphere, then heated to 1,500°C at a temperature increasing rate
of 10 °C/min, and maintained for 10 minutes. The obtained carbon fibers were found
to have a fiber diameter of about 9 µm.
(Example 3-1)
[0082] Carbon fibers according to Example 3-1 were produced in the same manner as in Example
2-1 except that the diameter of the nozzle holes of a wet-type spinning device was
changed to obtain polyoxazine/PBB=1/3 carbon fiber precursor fibers having a fiber
diameter of 20 µm. The obtained carbon fibers were found to have a fiber diameter
of about 16 µm.
(Example 3-2)
[0083] Carbon fibers according to Example 3-2 were produced in the same manner as in Example
3-1 except that the carbonization temperature was changed, i.e., the polyoxazine/PBB=1/3
carbon fiber precursor fibers were carbonized by being heated at 240°C for 30 minutes
in a nitrogen atmosphere, then heated to 1,500°C at a temperature increasing rate
of 10 °C/min, and maintained for 10 minutes. The obtained carbon fibers were found
to have a fiber diameter of about 12 µm.
(Comparative Example 1-1)
[0084] Carbon fibers according to Comparative Example 1-1 were produced in the same manner
as in Example 1-1 except that the composition of the raw liquid for spinning was changed;
i.e., the raw liquid for spinning used was prepared by dissolving only 50 g of PBB
in 1 L of the methanesulfonic acid, and that the heat treatment at 240°C for 30 minutes
was not performed and the carbonization was performed by heating from room temperature
to 1,300°C at a temperature increasing rate of 10 °C/min and maintaining for 10 minutes.
The obtained carbon fibers were found to have a fiber diameter of about 9 µm.
(Comparative Example 1-2)
[0085] Carbon fibers according to Comparative Example 1-2 were produced in the same manner
as in Comparative Example 1-1 except that the carbonization temperature was changed,
i.e., the carbon fiber precursor fibers were carbonized by being heated from room
temperature to 1,500°C at a temperature increasing rate of 10 °C/min in a nitrogen
atmosphere and maintained for 10 minutes. The obtained carbon fibers were found to
have a fiber diameter of about 9 µm.
(Properties and Evaluation of Carbon Fibers)
<Density>
[0086] Table 1 below presents densities of the carbon fibers calculated by the sink-float
method.
Table 1
Ex./Comp. Ex. |
Polyoxazine/PBB |
Carbonization temperature (°C) |
Precursor fiber diameter (µm) |
Carbon fiber diameter (µm) |
Density (g/cm3) |
Ex. 1-1 |
1/1 |
1,300 |
12 |
9 |
1.71 |
Ex. 1-2 |
1/1 |
1,500 |
12 |
9 |
1.72 |
Ex. 2-1 |
1/3 |
1,300 |
12 |
9 |
1.78 |
Ex. 2-2 |
1/3 |
1,500 |
12 |
9 |
1.76 |
Ex. 3-1 |
1/3 |
1,300 |
20 |
16 |
1.80 |
Ex. 3-2 |
1/3 |
1,500 |
20 |
16 |
1.79 |
Comp. Ex. 1-1 |
PBB only |
1,300 |
12 |
9 |
1.82 |
Comp. Ex. 1-2 |
PBB only |
1,500 |
12 |
9 |
1.81 |
[0087] As presented in Table 1 above, the carbon fibers according to Examples 1-1 to 3-2
have slightly low or almost equivalent densities as compared with the carbon fibers
according to Comparative Examples 1-1 and 1-2. The densities of the carbon fibers
according to Examples 1-1 to 3-2 are almost equivalent to the densities of commercially
available PAN-type carbon fibers which are about 1.76 to about 1.81. Therefore, the
carbon fibers according to Examples 1-1 to 3-2 can be produced to have equivalent
densities to those of the practical products.
[0088] Also, the carbon fibers according to Examples 1-1 to 3-2 can be made thicker to have
a diameter of 9 µm or 16 µm, as compared with the diameters of commercially available
carbon fibers which are 5 µm to 7 µm.
-Crystallinity and Orientation-
[0089] Strength and elasticity of a carbon fiber depend on crystallinity and orientation
of graphite crystals constituting the carbon fiber.
[0090] Here, first, plane interval c/2 of carbon network planes and stack thickness L
c of carbon network planes were measured as parameters indicating crystallinity of
graphite crystals. FIG. 2A is a conceptual diagram indicating plane interval c/2 of
carbon network planes and stack thickness L
c of carbon network planes in a graphite crystal. Note that, reference signs 1a, 1b
and 1c in FIG. 2A denote carbon network planes.
[0091] The measurement of the plane interval c/2 of carbon network planes and the stack
thickness L
c of carbon network planes was performed by measuring a wide angle X-ray diffraction
profile with an X-ray diffraction device using CuKα rays monochromatized with a Ni
filter as an X-ray source. Specifically, in the optical system for an equatorial direction
illustrated in FIG. 2B, the plane interval c/2 of carbon network planes and the stack
thickness L
c of carbon network planes were obtained from the peak of plane index (002) observed
at 2θ of about 26° in the equatorial direction profile. Note that, FIG. 2B is a conceptual
diagram indicating an optical system in measuring a wide angle X-ray diffraction profile,
where the equatorial direction is a direction in which the detector is perpendicular
to the fiber axis and the meridional direction is a direction in which the detector
is in parallel with the fiber axis. Further, azimuth measurement is performed by rotating
the fiber from the meridional direction via the equatorial direction to the meridional
direction to obtain a profile of its X-ray intensity distribution in a state where
the detector is fixed at 2θ of about 26° using the X-ray diffraction device.
[0092] Next, orientation degree f of the graphite crystals obtained from the above-described
azimuth measurement is used as an index of a carbon fiber having practical strength
and elastic modulus. Note that, this orientation degree f is referred to as a practical
orientation degree, and in the case of carbon materials, it is calculated from the
formula: f = (1- H°/180) × 100, where (H°) denotes a full-width at half maximum of
the intensity distribution measured along a so-called Debye ring of the 002 plane
reflection of the graphite crystals observed at 2θ of about 26°. In FIG. 2A, the case
where f = 100 means that the carbon crystal network planes are all arranged in the
fiber axis direction, and the case where f = 0 means that the carbon crystal network
planes are arranged randomly with respect to the fiber axis direction.
[0093] Table 2 below presents the plane interval c/2 of the carbon network planes, the stack
thickness L
c of the carbon network planes, and the orientation degrees (f) of the graphite crystals
in the carbon fibers according to Examples 1-2, 2-2, and 3-2 and the carbon fibers
according to Comparative Example 1-2, which were carbonized at the carbonization temperature
of 1,500°C, and the PAN-type carbon fibers and the pitch-type carbon fibers. Note
in Table 2 below that, "*" means that the indicated values are the numerical values
disclosed in Referential Document 1.
[0094] Referential Document 1; A. Takaku, et al., J. Mater. Sci., 25, 4873 (1990)
Table 2
Ex./Comp. Ex. |
c/2 |
Lc |
f |
Ex. 1-2 |
0.351 |
1.68 |
77.2 |
Ex. 2-2 |
0.348 |
1.87 |
78.8 |
Ex. 3-2 |
0.342 |
1.88 |
77.3 |
Comp. Ex. 1-2 |
0.349 |
1.86 |
80.8 |
Commercially available PAN-type carbon fibers* |
0.350 |
2.31 |
84.2 |
Commercially available pitch-type carbon fibers* |
0.351 |
4.93 |
79.5 |
[0095] As presented in Table 2 above, the values of the plane interval c/2 of the carbon
network planes, the stack thickness L
c of the carbon network planes, and the orientation degrees f of the carbon fibers
according to Examples 1-2, 2-2, and 3-2 are equivalent to those of the carbon fibers
according to Comparative Example 1-2 derived from PBB, indicating that the carbon
fibers excellent in mechanical strengths can be produced at a lower cost.
[0096] Also, the values of the plane interval c/2 of the carbon network planes and the orientation
degrees f of the carbon fibers according to Examples 1-2, 2-2, and 3-2 are high values
comparable to those of PAN-type carbon fibers and pitch-type carbon fibers.
Reference Signs List
[0097]
- 1a, 1b, 1c
- carbon network planes
- c/2
- plane interval of carbon network planes
- Lc
- stack thickness of carbon network planes